disturbed orbit
... 卫星轨道satellite orbit 受摄轨道disturbed orbit 卫星轨道升交点ascending node of satellite orbit ...
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最后使用两层微分修正方法将圆型限制性三体问题模型下设计的轨道转换到受摄三体问题模型下。
Finally, the two level differential corrections method was proposed to transform the orbit designed under the circular restricted three-body problem model into the perturbed three-body problem model.
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